| タイトル | Aircraft Sensor Platform Has Increased Angular Range |
| 著者（英） | Bhardwaj, Suneel; Dabney, Philip W. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1995-04-01 |
| 言語 | eng |
| 内容記述 | Mechanism rotates and translates instrument platform within pressure housing in aircraft to aim remote-sensing instrument toward target on ground below. Enables instrument to look under aircraft structure at larger fore and aft angles without having to deploy instrument into air stream outside. Also provides 10 degrees of yaw compensation, reducing further need for adjustment of attitude of aircraft to keep target in sight. With yaw compensation, pilot can fly with wings level and nose pointed into crosswind while on desired flight path over target. |
| NASA分類 | MECHANICS |
| レポートNO | 95B10184
GSC-13624 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/305896 |
